EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 188-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
SECTION
COMPLIANCE CHECK
PASS
FAIL
VFR Installations – The portion of the cockpit placard that permits
IFR is obliterated. Add the following placard in full view of the
pilot, stating “Operation of This Aircraft is Limited to VFR Only” in
the same location as the obliterated statement or near the EFD1000
E5, in the same font size as the other placards in the cockpit. :
Verify the GPS connected to the EFD1000 E5 is labeled “GPS1” and if
a NAV receiver is connected it is labeled “VLOC1”.
Cessna 190/195 Aircraft s/n 16083 and below only, verify the
TAPES are configured to LOCKED OFF, and the original airspeed
indicator and altimeter are in the standard “T” arrangement.
Backup Nav Indicator (if required) connected to a nav source
installed in pilot’s field of view. The indicator must function if the
EFD and/or ACU circuit breaker is pulled
7.2
Circuit breaker installed for the EFD and ACU.
Verify no wiring/cabling from the backup turn and bank, altimeter,
or airspeed indicator is routed directly behind the fan on rear of the
EFD1000 E5 display.
6.9.4
RSM location are <2 degrees of needle deflection on hand held
compass within 18”x18”x18” survey area
1.1
Verify RSM is P/N 900-00003-00x Rev E or later
EFD braided ground strap is installed between unit and panel, RSM
ground wire attached to ground stud, RSM doubler/mounting plate
bonded to airframe ground and ACU(s) chassis bonded to airframe
ground. All measure no greater than .003 ohms to ground.
7.2
Wires, cables, and connectors clearly marked or stamped
7.2
EFD master switch and/or circuit breaker must be accessible to
flight crew and clearly marked.
11
Post Installation Operational Check
11.4
Document successful completion of Operational Check in aircraft
log book per FAR 91.407b
6.3
Log book entry stating aircraft has been modified in accordance
with EFD1000 E5 AML-STC.
1.10
Update warranty records on Aspen Avionics website at
www.aspenavionics.com/dealerramp
Misc
Complete the Installed Equipment Configuration Matrix in the E5
AFMS (900-00038-001) and insert the completed AFMS in the
Airplane Flight Manual. (See sample Appendix C)
Operation of This Aircraft is
Limited to VFR Only
See EFD1000 E5 AFMS
